Distributed electric tip fans for distortion tolerance of turbofan engines
US-2024209796-A1 · Jun 27, 2024 · US
US8935853B2 · US · B2
| Field | Value |
|---|---|
| Publication number | US-8935853-B2 |
| Application number | US-201314102769-A |
| Country | US |
| Kind code | B2 |
| Filing date | Dec 11, 2013 |
| Priority date | Jul 5, 2006 |
| Publication date | Jan 20, 2015 |
| Grant date | Jan 20, 2015 |
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An exemplary turbine engine assembly includes a first shaft that is rotatably driven by a second shaft of a gas turbine engine, a compressor hub driven by the second shaft, the compressor hub within a compressor section of the gas turbine engine, an epicyclic gear train that is driven by the first shaft, and a common attachment point that secures the first shaft and the compressor hub to the second shaft.
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What is claimed is: 1. A turbine engine assembly comprising: a first shaft that is rotatably driven by a second shaft of a gas turbine engine; a compressor hub driven by the second shaft, the compressor hub within a compressor section of the gas turbine engine; an epicyclic gear train that is driven by the first shaft; and a common attachment point that secures the first shaft and the compressor hub to the second shaft. 2. The turbine engine assembly of…
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